Ni—Ti—CR near ternary eutectic alloy for gas turbine component repair
A ternary near eutectic alloy of Ni, Ti, Cr is described having a relatively low melting temperature of approximately 1230 deg. C. or less, suitable for fusing cracks in turbine blades and vanes without substantial risk of cracking during the repair process. Such an alloy is suitable for low temperature joining or repair of turbine blades since it contains the same components as typical turbine blades and vanes without foreign elements to lower the melting point of the repaired material or adversely affect the mechanical properties of the repaired component. Exclusion of boron eliminates the formation of brittle boron compounds, detrimental to the properties of the repair or seam.
1. A ternary near eutectic alloy consisting of 60 weight percent nickel, 20 weight percent titanium and 20 weight percent chromium and having a melting temperature less than 1230 deg. C. and therefore suitable for joining or repair of superalloy gas turbine components.
2. A ternary alloy consisting of nickel, titanium and chromium wherein said nickel is present in an amount in the range from approximately 55 to approximately 65 weight percent, and said titanium is present in an amount in the range from approximately 15 to approximately 25 weight percent, and said chromium is present in an amount in the range from approximately 15 to approximately 25 weight percent, and the alloy has a melting temperature greater than a melting temperature of a ternary eutectic alloy of the same constituents and less than 1230 deg. C.
3. The ternary alloy as in claim 2 wherein said nickel is present in an amount of approximately 60 weight percent, said titanium is present in an amount of approximately 20 weight percent and said chromium is present in an amount of approximately 20 weight percent.
4. The ternary alloy as in claim 2 wherein the alloy is a braze alloy.